N386AA

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 84,353 hrs · 13,497 cycles

CABIN PRESSURIZATION LOST AT FL 370. EMERGENCY DECENT ACCOMPLISHED NO MASKS DEPLOYED. DIVERTED, EMERGENCY DECLARED, AND LANDED UNEVENTFULLY. REPLACED CABIN ALTITUDE PRESSURE CONTROLLER IAW MM 21-31-00. ACCOMPLISHED CABIN CONTROLLER BITE TEST IAW MM 21-31-00. NO FAULT NOTED. ACCOMPLISHED ACFT PRESSURIZATION IAW MM 21-31-01, FOUND NORMAL.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 83,405 hrs · 13,333 cycles

SEAT 5B FWD SEAT MOUNTED EMER LIGHT INOPERATIVE. SECURED CONNECTOR AT LIGHT ASSEMBLY. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 82,973 hrs · 13,272 cycles

SEAT 5B EMER LIGHT INOPERATIVE. REPLACED LAMP. OPERATIONS CHECKED NORMAL.

Part: SKIN PANEL — DELAMINATED (VERTICAL STAB) · airframe 82,506 hrs · 13,189 cycles

VERTICAL STABILIZER LT SIDE HAS AN AREA OF DELAMINATION ON THE SIDE SKIN CENTERED 63 INCHES FROM THE LE & 58 INCHES UP FROM THE FUSELAGE. PANEL REPAIRED IAW EA B767-55-035420.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 82,506 hrs · 13,189 cycles

HOLE DAMAGE UNDER DOUBLER AT VERY BOTTOM HOLE IN FWD BOTTOM CORNER OF DOUBLER. INSTALLED OVERSIZED FASTENERS IAW EA B767-53-035619.

Part: PANEL — DAMAGED (FUSELAGE) · airframe 82,506 hrs · 13,189 cycles

PANEL DAMAGED AT BS 246 & RBL 12. INSTALLED DOUBLER IAW SRM 53-10-51-2R-5 & EA B767-53-035664.

Part: SKIN — MECHANIC ERROR (FUSELAGE) · airframe 82,506 hrs · 13,189 cycles

DOUBLER AT STATION 1210 & STRINGER 34L IS AN IMPROPER DOUBLER FOR CIRCUMFERENTIAL BUTT SPLICE AREA IAW SRM 53-00-01-2R-1. REPLACED DOUBLER IAW EA B767-53-035619.

Part: STRINGER — DEFECTIVE (FUSELAGE) · airframe 82,506 hrs · 13,189 cycles

STRINGER 34 LT AT STATION 1210 HAS TWO DEFECTIVE FASTENER HOLES THAT WAS USED TO SECURE FILLER FOR SKIN REPAIR. HOLES ARE WITHIN 10 INCHES OF A PRODUCTION STRINGER SPLICE. INSTALLED STRINGER & SPLICE IAW EA B767-53-035619.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 82,506 hrs · 13,189 cycles

RIGHT COACH EMER PATH LIGHTS FAILED TESTING. REPLACED BATTERY PACK M210. OPERATIONS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 82,506 hrs · 13,189 cycles

LEFT COACH EMER PATH LIGHTS FAILED TESTING. REPLACED BATTERY PACK M738. OPERATIONS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 82,506 hrs · 13,189 cycles

LEFT COACH EMER PATH LIGHTS FAILED TESTING. REPLACED BATTERY PACK M739. OPERATIONS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 82,506 hrs · 13,189 cycles

RIGHT COACH EMER PATH LIGHTS FAILED TESTING. REPLACED BATTERY PACK M732. OPERATIONS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 82,506 hrs · 13,189 cycles

LEFT COACH EMER PATH LIGHTS FAILED TESTING. REPLACED BATTERY PACK M737. OPERATIONS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 82,506 hrs · 13,189 cycles

RIGHT COACH EMER PATH LIGHTS FAILED TESTING. REPLACED BATTERY PACK M733. OPERATIONS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 82,506 hrs · 13,189 cycles

EMERGENCY LIGHTS FROM SEATS 32JH TO 41JH INOPERATIVE. REPLACED BATTERY PACK M734 FOR EMER LIGHTS FROM SEATS 32JH TO 41JH. OPERATIONS CHECKED NORMAL.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 82,506 hrs · 13,189 cycles

CORROSION FOUND ON AFT CARGO FLOORBEAM J CHORD AT STATION 1153. R & R J CHORD IAW AARD 51-00-05, DWGS 146T1204 ID 0001 REV F & 146T5000 ID 0007 REV B.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 82,506 hrs · 13,189 cycles

HORIZONTAL STAB LT SIDE STATION 1809.5, FOUR EACH FASTENER HOLES OPEN FOR INSPECTION OF FWD OUTER CHORD FOR CRACKS. THE FWD LOWER HOLE & AFT UPPER HOLE, HAVE EXCESSIVE SIGNAL TO NOISE INDICATIONS. REAMED .2755 2ND OVER & INSTALLED FASTENERS IAW EA B767-53-035570.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,144 hrs · 13,112 cycles

AFT LT FUSELAGE SKIN IS CORRODED AT STATION 1210 & STRINGER 34 LT. ACCOMPLISHED DOUBLER REPAIR IAW SRM 53-00-01-2R-1.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 81,762 hrs · 13,048 cycles

EMERGENCY LIGHT AT SEAT 26H INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 26H, OPERATIONS CHECKED NORMAL.

Part: ROTARY ACTUATOR — MALFUNCTIONED (TE FLAP) · airframe 77,640 hrs · 12,385 cycles

SFO - CREW REPORTED "TE FLAP DISAGREE" EICAS MESSAGE WHEN FLAPS 5 DEGREES SELECTED. ACCOMPLISHED QRH CHECKLIST. EMERGENCY DECLARED FLIGHT LANDED WITHOUT INCIDENT. FOUND NUMBER SEVEN ROTARY ACTUATOR OVERTORQUE INDICATOR POPPED. REPLACED NUMBER SEVEN FLAP ROTARY ACTUATOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: ACTUATOR — TRIPPED (TE FLAP) · airframe 77,640 hrs · 12,385 cycles

JFK - CREW REPORTED TRAILING EDGE FLAP DISAGREE MESSAGE WITH TRAILING EDGE FLAP LIGHT. EMERGENCY DECLARED FLIGHT LANDED JFK WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. RESET NUMBER SEVEN ACTUATOR THAT HAD TRIPPED. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SENSOR — INOPERATIVE (LE SLAT) · airframe 77,553 hrs · 12,370 cycles

JFK - CREW REPORTED LEADING EDGE SLAT DISAGREE MESSAGE DURING APPROACH. EMERGENCY DECLARED FLIGHT LANDED JFK WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED SENSOR S285. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: ACTUATOR — FAILED (NR 5 SPOILER) · airframe 76,142 hrs · 12,149 cycles

GRU - CREW REPORTED CENTER HYDRAULIC SYSTEM FAILED. EMERGENCY DECLARED FLIGHT RETURNED GRU LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NUMBER 5 SPOILER ACTUATOR AT LEFT WING. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: TRANSCEIVER — FAILED (WEATHER RADAR) · airframe 75,982 hrs · 12,123 cycles

DFW - (REPEAT ITEM) CREW REPORTED BOTH WEATHER RADAR SYSTEMS FAILED DURING CRUISE. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED WEATHER RADAR TRANSCEIVER AND ANTENNA. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CONTROL PANEL — INOPERATIVE (WEATHER RADAR) · airframe 75,947 hrs · 12,118 cycles

DFW - CREW REPORTED WEATHER RADAR FAILED. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED WEATHER RADAR CONTROL PANEL. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LENS — MISSING (CABIN) · airframe 75,808 hrs · 12,098 cycles

SEAT MOUNTED EMERGENCY LIGHT AT 21H MISSING LENS. REPLACED LIGHT ASSEMBLY FOR SEAT MOUNTED EMERGENCY LIGHT AT 21H. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 75,808 hrs · 12,098 cycles

SEAT MOUNTED EMERGENCY LIGHT AT 21H INOPERATIVE. REPLACED LAMPS FOR SEAT MOUNTED EMERGENCY LIGHT AT 21H. OPS CHECK NORMAL.

Part: CONTROL UNIT — INOPERATIVE (ANTI-SKID SYS) · airframe 75,552 hrs · 12,053 cycles

JFK - CREW REPORTED ANTI-SKID INOPERATIVE. EMERGENCY DECLARED FLIGHT LANDED JFK WITHOUT INCIDENT. REPLACED ANTI SKID/ AUTO BRAKE CONTROL UNIT. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 75,323 hrs · 12,014 cycles

RIGHT 1 DOOR EMERGENCY EXIT SIGN THRESHOLD LIGHT HAS ONE BULB INOPERATIVE. REPLACED LAMP FOR RIGHT NUMBER 1 DOOR EMERGENCY EXIT SIGN THRESHOLD LIGHT. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 75,323 hrs · 12,014 cycles

LEFT NUMBER 1 DOOR EMERGENCY EXIT SIGN THRESHOLD LIGHT HAS ONE BULB INOPERATIVE. REPLACED LAMP FOR LEFT NUMBER DOOR 1 EMERGENCY EXIT SIGN THRESHOLD LIGHT. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,332 hrs · 11,846 cycles

RIGHT NUMBER 1 DOOR SLIDE EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR RIGHT NUMBER 1 DOOR SLIDE EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: FITTING — CRACKED (RT WING) · airframe 72,099 hrs · 11,508 cycles

CRACK AT FORWARD TENSION BOLT HOLES ON THE RIGHT WING AFT PITCHLOAD FITTING, OUTBOARD HOLE ONLY. ACCOMPLISHED REPAIR PER EA B767-57-017927.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,099 hrs · 11,508 cycles

CORROSION WAS FOUND ON STATION 347 FLOORBEAM UPPER CAP HORIZONTAL FLANGE UPPER SURFACE. THE AREAS OUT LIMITS WERE AT RIGHT BUTTLINES 46.5 TO 65.5, REMOVED ALL CORROSION PER 767-300 SRM 51-10. FABRICATED REPAIR PARTS STRAPS, APPLIED ALODINE AND TWO COATS OF PRIMER. FILLED ALL BLENDS WITH BMS 5-95 AND INSTALLED ALL REPAIR PARTS PER EA B767-53-017746.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,099 hrs · 11,508 cycles

CORROSION WAS FOUND AT STATION 325 FLOORBEAM UPPER CAP HORIZONTAL FLANGE UPPER SURFACE. THE OUT OF LIMITS WERE AT LEFT BUTTLINE 17 AND RIGHT BUTTLINE 31. REMOVED ALL CORROSION PER 767-300 SRM 51-10. FABRICATED REPAIR STRAPS, APPLIED ALODINE AND PRIMER, FILLED ALL BLENDS WITH BMS 5-95. INSTALLED ALL REPAIR PARTS AND APPLIED TWO COATS OF CIC TO ENTIRE REPAIR AREA PER E.A B767-53-017747.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 72,099 hrs · 11,508 cycles

GOUGES WERE FOUND AT STATION 1562 FLOORBEAM UPPER CAP HORIZONTAL FLANGE UPPER SURFACE. REMOVED ALL GOUGES, FABRICATE PARTS, APPLY ALODINE, TWO COATS OF PRIMER AND ACCOMPLISHED A GVI WITH IN 22 INCHES OF THE REPAIR AREA, APPLY TWO COATS OF CIC TO ENTIRE REPAIR AREA. ACCOMPLISHED REPAIR PER EA B767-53-017777.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 3 · airframe 72,099 hrs · 11,508 cycles

CORROSION WAS FOUND ON FORWARD CARGO DOOR LOWER SILL FAIL SAFE STRAP AND OUTER CHORD. REMOVED CORROSION PER SRM, ACCOMPLISHED HFEC TO SURFACE ALL BLENDED AREAS, ACCOMPLISHED OPEN HOLE HFEC INSPECTION ON ANY FASTENER HOLE, ACCOMPLISHED VISUAL INPECTION WITHIN 22 INCHES OF DAMAGE. ALODINED, PRIMED AND INSTALLED WITH PRODUCTION TYPE FASTENERS AND APPLY CIC TO ENTIRE REPAIR AREA. REFERENCE EA B767-53-017706 FOR COMPLETE DESCRIPTION AND REPAIR INSTRUCTIONS.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 67,357 hrs · 10,713 cycles

SEAT 27H EMERGENCY LIGHT INOPERATIVE. RE-SECURED CONNECTOR FOR SEAT 27H EMERGENCY LIGHT. OPS CHECKED NORMAL.

Part: GUARD — DAMAGED (CABIN) · airframe 67,357 hrs · 10,713 cycles

SEAT 30H EMERGENCY LIGHT GUARD DAMAGED. REPLACED GUARD FOR EMERGENCY LIGHT AT SEAT 30H. OPS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,357 hrs · 10,713 cycles

LEFT NUMBER 1 DOOR EXIT LIGHT ONE FLOOD LIGHT INOPERATIVE. REPLACED LAMP FOR FLOOD LIGHT AT LEFT NUMBER 1 DOOR. OPS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,357 hrs · 10,713 cycles

LEFT NUMBER 2 DOOR EXIT LIGHT ONE FLOOD LIGHT OUT. REPLACED LAMP FOR FLOOD LIGHT AT LEFT NUMBER 2 DOOR. OPS CHECKED NORMAL.

Part: PRESSURE BLKHD — FAULTY (HYDRAULIC SYS) · airframe 67,055 hrs · 10,660 cycles

BOS - CREW REPORTED CENTER HYDRAULIC SYSTEM PRESSURE WARNING LIGHT ILLUMINATED DURING FLIGHT. EMERGENCY DECLARED RETURNED BOS LANDED WITHOUT INCIDENT. REPLACED CENTER HYDRAULIC PRESSURE SWITCH. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SIGN — LOOSE (CABIN)

MIA EMERGENCY EXIT SIGN LOOSE ABOVE SEAT 42C. RESECURED EMERGENCY EXIT SIGN ABOVE SEAT 42C.

Part: STATOR — FAILED (NR 1 RPM) · airframe 62,588 hrs · 9,915 cycles

JFK INFLIGHT ORD TO MAN - CREW REPORTED NR 1 ENGINE HIGH PRESSURE ROTOR SPEED INDICATION FAILURE ACCOMPANIED BY LEFT CENTER FUEL PUMP PRESSURE LIGHT. IN DESCENT AT IDLE THRUST LEFT OIL PRESSURE INDICATION TURNED AMBER WITH 33 PSI. LANDED JFK WITHOUT INCIDENT. SUSPECT THE HIGH PRESSURE ROTOR SPEED TACH CONTROL ALTERNATOR STATOR FAILED. REPLACED NR 1 ENGINE ROTOR AND STATOR. ALSO, REPLACED NR 1 ENGINE HIGH PRESSURE ROTOR SPEED CARD. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 60,670 hrs

BOS SEAT MOUNTED EMERGENCY LIGHT AT SEAT 6B INOPERATIVE. SECURED CONNECTOR FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 6B. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 60,099 hrs

SFO - EXTERIOR EMERGENCY LIGHT AT LT NR FOUR DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT LT NR FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: PIN — MISSING (EMERGENCY LIGHTS)

MIA - EMERGENCY LIGHT AT SEAT 4AB DAMAGED. REPLACED PIN FOR EMERGENCY LIGHT AT SEAT 4AB. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — DAMAGED (CABIN) · airframe 59,526 hrs

ORD - EMERGENCY LIGHT AT SEAT 4B HIT BY PASSENGER BAG AND SEPARATED FROM SEAT. RESECURED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 4B. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ACTUATOR — LEAKING (NR 10 SPOILER) · airframe 59,027 hrs

MAN INFLIGHT T55/23FEB - CREW REPORTED CENTER HYDRAULIC SYSTEM FLUID LOSS. RETURNED TO MAN AND LANDED WITHOUT INCIDENT. REPLACED NR 10 SPOILER ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 58,456 hrs

JFK - EMERGENCY LIGHT AT OVERHEAD AFT GALLEY INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD AFT GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

ORD - EMERGENCY LIGHT AT SEAT 21F INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 21F. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SWITCH — INOPERATIVE (EMERGENCY LIGHTS)

ORD - EMERGENCY LIGHTS IN CABIN TURN ON WITH SWITCH OFF. REPLACED FORWARD FLIGHT ATTENDANTS SWITCH FOR EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: MODULE — INOPERATIVE (EMERGENCY LIGHT)

MIA - EMERGENCY LIGHTS AT SEAT ROWS 32H TO 35H INOPERATIVE. RESET MODULE FOR EMERGENCY LIGHTS AT SEAT ROWS 32H TO 35H. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SKIN — WORN (LT WING)

AFW - LEFT WING LOWER SKIN SURFACE AT APPROXIMATELY WING STATION 602 AND JUST AFT OF STRINGER 66 UNDER FAIRING FOR OUTBOARD FLAP HAS TWO WORN AREAS. AREA OF DISCREPANCY IS 0.7 INCHES BY 1.0 INCHES AND 7 INCH DIAMETER WITH .005 DEPTH. BLENDED AREA UNTIL SMOOTH AND PERFORM HIGH FREQUENCY EDDY CURRENT INSPECTION FOR CRACKS. ROTO PEENED AREA AND REFINISH WITH ALODINE AND TWO COATS OF BMS 10 79 PRIMER.

Part: WIRE HARNESS — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT ROW 39H INOPERATIVE. FOUND LOOSE CONNECTION. RESECURED LOOSE CONNECTION. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - ALL FOUR EMERGENCY LIGHT OVERWING EXIT SIGNS INOPERATIVE. REPLACED BATTERY PACK M1209 FOR ALL FOUR EMERGENCY LIGHT OVERWING EXIT SIGNS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SPAR — CORRODED (WING)

AFW - REAR SPAR WEB WING CENTER SECTION OUTBOARD SIDE OF THE INBOARD LEG OF THE PICKLE FORK HAS BLEND IN AREA APPROXIMATELY 3 INCH BY 0.5 INCH WITH A DEPTH OF 0.067 INCH. REMOVED EXPOSED CORROSION FROM THE REAR SPAR SURFACE. UNDERCUT THE SPAR AND PICKLE FORK APPROXIMATELY ONE EIGHTH INCH TO REMOVE ANY POSSIBLE CORROSION UNDER THE PICKLE FORK. PERFORMED A DETAILED VISUAL INSPECTION TO ENSURE CORROSION WAS REMOVED. ALODINED, PRIMED, AND APPLIED LIBERAL AMOUNTS OF BMS 335.

Part: LIGHT — MELTED (COCKPIT)

SMOKE FROM GEAR HANDLE SLOT ON SHORT FINAL AFTER GEAR CONFIRMED DOWN LOCKED. LEFT GEAR LIGHT WENT OUT. SMOKE FOR 10 SECONDS. LANDING NORMAL. REPLACED LEFT MAIN GEAR ANNUNCIATOR LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PIN — BROKEN (EMERGENCY LIGHT)

JFK EMERGENCY LIGHT ON THE SIDE OF ROW 39H INOPERATIVE. REPAIRED BROKEN CONTACT PIN FOR EMERGENCY LIGHTS AT SEAT 39H. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: CONNECTOR — BROKEN (EMERGENCY LIGHTS)

ORD - EMERGENCY LIGHTS AT SEAT 22B INOPERATIVE. REPLACED BROKEN CONNECTOR AT SIDEWALL PANEL FOR EMERGENCY LIGHTS AT SEAT 22B. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2

AFW CORROSION FOUND ON 1.5 BY .7 INCH AREA, DEPTH .040, OF FORWARD CARGO DOOR LOWER MAIN SILL NEAR STA 613. THICKNESS PRIOR TO CORROSION REMOVAL WAS .276. REMOVED FASTENERS AS REQUIRED FOR BLENDOUT. ENSURE NO CORROSION ON FASTENERS OR IN HOLES. REMOVED ALL CORROSION. INSPECTED USING HFEC FOR CRACKS. ROTO-PEEN BLENDED SURFACES. ALODINE AND PRIME BLENDED AREA WITH TWO COATS PRIMER. APPLIED DYNOL TO ENTIRE AREA. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — DISCONNECTED (CABIN)

DURING OVERNIGHT MAINTENANCE FOUND EMERGENCY ESCAPE LIGHTING AT SEAT 7B, INOPERATIVE. RECONNECTED LOOSE SEAT ROW CONNECTOR AT SEAT 7B. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: POWER SUPPLY — DISCHARGED (CABIN)

EZE - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTING FOR RIGHT SEATS 32 THROUGH 41 INOPERATIVE. REPLACED EMERGENCY ESCAPE PATH LIGHT POWER SUPPLY M739. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: GCU — FAILED (E/E BAY)

JFK - FLT 182 - AFTER 40 MINUTES OF FLIGHT LEFT GENERATOR OFF, WOULD NOT RESET. REMOVED AND REPLACED LEFT GCU AND LEFT IDG. PERFORMED OPERATIONAL CHECK OF LEFT GENERATOR SYSTEM. ALL OPS NORMAL. PERFORMED ENGINE RUN SYSTEM CHECKS NORMAL. NO LEAKS NOTED. OK FOR SERVICE. (M)

Part: BATTERY PACK — INOPERATIVE (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTS AT 7AB AND 1-8 INOPERATIVE. REPLACED EMERGENCY ESCAPE PATH LIGHTS BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FIRE WARNING — FALSE INDICATION (LAVATORY)

SFO - FLT 11 - EN ROUTE SFO-JFK - FIRE WARNING INDICATION LIGHT ILLUMINATED FOR AFT LAVATORY. RETURNED SFO AND LANDED WITHOUT FURTHER INCIDENT. INSPECTED LAVATORY WIRING, PLUMBING, AND COMPONENTS. RAN BOTH ENGINES AND PACKS. NO FAULTS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — DAMAGED (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT L1 DOOR INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE AT SEAT 2B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — BROKEN (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EXIT LIGHT AT 22B INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE AT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SOCKET — DIRTY (CABIN)

LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT INOPERATIVE. CLEANED EMERGENCY EXIT LIGHT SOCKET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: PACKING — DEFECTIVE (CABIN)

DFW - FLT 1539 - EN ROUTE MIA-SFO, DETECTED WATER COMING DOWN AT CENTER OF CABIN. TURNED OFF ALL VIDEO MONITORS. DIVERTED DFW AND LANDED WITHOUT FURTHER INCIDENT. REPLACED LEFT WATER EXTRACTOR PACKING. LEAK CHECKS GOOD. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — INOPERATIVE (CABIN)

LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 28B INOPERATIVE. RE-SEATED EMERGENCY EXIT LIGHT CONNECTOR AT SIDE WALL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — INOPERATIVE (CABIN)

LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 2B INOPERATIVE. RE-CONNECTED EMERGENCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — DISCONNECTED (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 22B INOPERATIVE. RE-CONNECTED EMEREGNCY EXIT LIGHT CONNECTOR AT SEAT 22B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — BROKEN (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHT AT SEAT 36H INOPERATIVE. REPAIRED CONNECTOR AT SEAT 36H. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: CONNECTOR — DAMAGED (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EXIT LIGHT AT SEAT 35H INOPERATIVE. RE-PINNED SEAT MOUNTED EMERGENCY EXIT CONNECTOR AT SEAT 35H. SYSTEM GROUND CHECKED NORMAL OPS. (M)

Part: CONNECTOR — DISCONNECTED (SEAT 23)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT PATH LIGHT AT SEAT 23H INOPERATIVE. RECONNECTED EMERGENCY EXIT SEAT PATH LIGHT CONNECTOR AT SEAT 23H. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: FLOORBEAM — CORRODED (BS 1480)

AFW - FLOORBEAM AT STATION 1480 HAD CORROSION ON TOP SURFACE BLENDED BEYOND SRM LIMITS. FABRICATE REPAIR STRAP OF 301.5H SS .050 INCH CHICK. ALODINE ALL BARE ALUM SURFACES, FINISH BLENDS AND REPAIR PARTS W/2 COATS BMS 10-11 PRIMER FILL BLENDS WITH BMS 5-92. INSTALL STRAP WET W/BMS 5-95. PROSEAL 870 MRB767-1983. (M)

Part: FLOORBEAM — CORRODED (BS 792-827)

AFW - FOUND CORROSION IN THE UPPER CHORD OF THE LBL 33 AND RBL 33 LONGITUDINAL FLOORBEAMS, AT BODY STATIONS 827 AND 792. VERIFY CORROSION COMPLETELY REMOVED AND BLENDED AREA IS CRACK FREE. ROTO PEEN BLENDED AREA. APPLY ALODINE AND 2 COATS PRIMER, FILL BLENDS WITH BMS5-95 SEALANT MRB 767-1981. (M)

Part: FLOORBEAM — CORRODED (BS 347)

AFW - FLOORBEAM AT STATION 347 HAD CORROSION ON TOP SURFACE BLENDED BEYOND SRM LIMITS. FABRICATE REPAIR STRAP OF 301..5H SS, .050 INCH THICK, ALODINE ALL BARE ALUM FINISH BLENDS AND REPAIR PARTS WITH 2 COATS BMS 10-11 PRIMER. FILL BLENDS W/BMS 5-92. INSTALL REPAIR STRAP WET W/BMS 5-95 SEALANT, PROSEAL 970 MRB REPAIR 767-1982. (M)

Part: FLOORBEAM — CORRODED (BS 347)

AFW - FLOORBEAM AT STATION 347 HAD AREAS OF CORROSION BLENDED BEYOND SRM LIMITS. FABRICATE REPAIR STRAP OUT OF 301.5 SS .050. ALODINE ALL BARE ALUM SURFACES FINISH BLENDS AND REPAIR PARTS WITH 2 COATS BMS 10-11 PRIMER. FILL BLENDS WITH BMS 5-92, INSTALL STRAP WET W/BMS 5-95 SEALANT, PROSEAL 870 REPAIR PER MRB 767-1980. (M)

Part: O-RING — TORN (NR 9 SPOILER)

ORD - FLT 84 - AFTER TAKEOFF ORD-FRA, CENTER HYDRAULIC SYSTEM LOST QUANTITY FOLLOWED BY LOSS OF PRESSURE. RESERVE BRAKES/STEERING SWITCH SELECTED FOLLOWING GEAR EXTENSION WHICH MOMENTARILY RESTORED PRESSURE. ALTERNATE FLAP EXTENSION PERFORMED. AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REPLACED O-RING IN NR 9 SPOILER ACTUATOR. ALSO, REPLACED AC MOTOR DRIVEN HYDRAULIC PUMPS, AIR DRIVEN HYDRAULIC PUMP, AND FILTERS AS PRECAUTIONARY MEASURE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — DAMAGED (ROW 38B)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHT AT SEAT ROW 38B INOPERATIVE. REPAIRED EMERGENCY EXIT SEAT LIGHT WIRING AT SEAT ROW 38B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — FAILED (SEAT 38HJ)

DFW - DURING OVERNIGHT CHECK, EMERGENCY EXI TLIGHT AT PAX SEAT 38HJ INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT CONNECTOR AT PAX SEAT 38HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — FAILED (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHTS AT SEAT 29HJ INOPERATIVE. REPLACED CONNECTOR AND HARNESS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — DEFECTIVE (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT PASSENGER SEAT 41H INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT SIDE WALL CONNECTOR AT PASSENGER SEAT ROW 41H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: IDG — FAILED (RIGHT)

JFK - FLT 0016 - DURING CRUISE AT FL 370, RIGHT GENERATOR DRIVE LIGHT BEGAN FLICKERING. A FEW MINUTES LATER, THE GENERATOR DRIVE MESSAGE ON THE EICAS CAME ON AND CREW DISCONNECTED THE IDG PER PROCEDURES. REPLACED RT IDG, RAN NR 2 ENGINE. ALL PARAMETERS NORMAL. LEAK CHECK OK. OK FOR SERVICE. 386242DC4/2155.18FEB.JFK. (X)

Part: CONNECTOR — LOOSE (RADAR SYSTEM)

GRU - FLT 0950 - DURING CLIMB AT FL 230, WX RADAR FAIL MSG BEGAN TO INTERMITTENTLY FLASH IN ALL MODES AND RANGES. AT FL 290, WX RADAR FAIL MSG WAS STEADILY ILLUMINATED IN ALL MODES AND RANGES. REPEAT WRITE-UP 97.98.99, AND 04. ACFT INSPECTED AND FOUND IN SAFE CONDITION FOR FERRY FLIGHT FROM GRU TO JFK FOR WEATHER RADAR SYSTEM MX EVALUATION. FERRY FLIGHT AUTHORIZED BY SPOTTING MESSAGE NR 02-162 DATED 2-26-97. CLEANED CONNECTORS ON WXR R/T AND ANTENNA. ACCOMPLISHED WEATHER RADAR BITE PER MM 34-7. NO FAULT NOTED. SYSTEM OK FOR SERVICE. NOTE: ACCOMPLISHED FOLLOW-UP BILL OF WORK JFK. FOUND WAVE GUIDE IMPROPERLY CONNECTED. CORRECTED WAVE GUIDE AND SYSTEM OPERATIONS FOUND NORMAL. (X)

Part: ANTENNA — FAILED (RADAR)

MIA - FLT 0907 - WX RADAR FAILED ONE HOUR INTO FLIGHT. SHOWS CORRESPONDING WX RADAR FAIL ANNUNCIATON ON HSI. T/S, REMOVED AND INSTALLED NEW WX RADAR ANTENNA PER MM. OPS CKS NORMAL. (X)

Part: CONNECTOR — DEFECTIVE (SEAT ROW 3H)

SFO - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT FLOOR PATH LIGHTING AT SEAT ROW 3H INOPERATIVE. REPLACED CONNECTOR AT SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)